JPS5886405U - Radial turbine nozzle support structure - Google Patents
Radial turbine nozzle support structureInfo
- Publication number
- JPS5886405U JPS5886405U JP18214181U JP18214181U JPS5886405U JP S5886405 U JPS5886405 U JP S5886405U JP 18214181 U JP18214181 U JP 18214181U JP 18214181 U JP18214181 U JP 18214181U JP S5886405 U JPS5886405 U JP S5886405U
- Authority
- JP
- Japan
- Prior art keywords
- nozzle
- support structure
- flange
- radial turbine
- attached
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第1図は従来め)シアルタービンノズルの支持構造の一
例を上半部のみ示す断面図、第2図は本考案ラジアルタ
ービンノズルの支持構造の一例を上半部のみ示す断面図
、第3図はそのタービンノズルを詳細に示す斜視図、第
4図はその支持ピンの形状を示す斜視図、第5図は本考
案の他の実施例を示す断面図、第6図AおよびBはその
支持ピンおよび板ばねの形状の一例を示すそれぞれ斜視
図である。
1・・・・・・ノズル翼、IA・・・・・・ノズル部、
2・・・・・・タービンロータ、3・・・・・・フラン
ジ部、4・・・・・・ホルダ、5・・・・・・スクロ=
ル、5A・・・・・・フランジ部、6−−−−−−ピン
、7・・・・・・ワッシャ、8・・・・・・ナツト、9
・・・・・・コイルばね、10・・・・・・タービンシ
ュラウド、11・・・・・・ベアリングハウジング、1
2・・・・・・軸受、13・・・・・・タービン軸、1
4. 15−−−−−−シールリング、21・・・・・
・ノズル翼、21A・・・・・・タービンノズル、22
・・・・・・フランジ、22A・・・・・・内周面、2
3・・・・・・切欠き溝、24・・・・・・段付き部、
i5・・・・・・支持ピン、25A・・・・・・頭部、
25B・・・・・・ばね止め部、26・・・・・・フラ
ンジ、27・・・・・・ベアリングハウジング(ノズル
取付部材)、27A・・・・・・内周面、28・・・・
・・ベアリングハウジング、29・・・・・・切欠き溝
、30・・・・・・ばね、31・・・・・・嵌め込み溝
、31A・・・・・・壁部、35・・・・・・ピン、3
5A・・・・・・頭部、35B・・・・・・軸部、35
C・・・・・・ばね止め部、36・・・・・・ばね。Fig. 1 is a sectional view showing only the upper half of an example of the support structure of a conventional radial turbine nozzle, Fig. 2 is a sectional view showing only the upper half of an example of the support structure of the radial turbine nozzle of the present invention, and Fig. 3 is a perspective view showing details of the turbine nozzle, FIG. 4 is a perspective view showing the shape of its support pin, FIG. 5 is a sectional view showing another embodiment of the present invention, and FIGS. 6A and B are its support. FIG. 3 is a perspective view showing an example of the shapes of a pin and a leaf spring, respectively. 1... Nozzle blade, IA... Nozzle part,
2...Turbine rotor, 3...Flange part, 4...Holder, 5...Scroll=
5A...Flange part, 6------Pin, 7...Washer, 8...Nut, 9
......Coil spring, 10...Turbine shroud, 11...Bearing housing, 1
2...Bearing, 13...Turbine shaft, 1
4. 15---Seal ring, 21...
・Nozzle blade, 21A...Turbine nozzle, 22
...Flange, 22A ...Inner peripheral surface, 2
3...Notch groove, 24...Stepped part,
i5...Support pin, 25A...Head,
25B... Spring stopper, 26... Flange, 27... Bearing housing (nozzle mounting member), 27A... Inner peripheral surface, 28...・
... Bearing housing, 29 ... Notch groove, 30 ... Spring, 31 ... Fitting groove, 31A ... Wall part, 35 ... ...Pin, 3
5A...Head, 35B...Shaft, 35
C...Spring stop part, 36...Spring.
Claims (1)
ラウドとの間にタービンロータへ4の高温ガス通路を形
成するフランジを有し、ノズル取付部材に取付けられた
ラジアルタービンノズルの支持構造において、前記フラ
ンジに係止溝を形成し、該係止溝に一端を係止させたピ
ンを、当該ピンの他端と前記ノズル取付部材との間に介
装した弾性部材により該ノズル取付部材側に付勢し°C
1前記フランジを前記ノズル取付部材に取付けたことを
特徴とするラジアルタービンノズルの支持構造。In a support structure for a radial turbine nozzle attached to a nozzle mounting member, the support structure includes a nozzle vane and a flange to which the nozzle vane is attached to form four high-temperature gas passages to the turbine rotor between the nozzle vane and a turbine shroud, and the flange is attached to the flange. A locking groove is formed, and a pin having one end locked in the locking groove is urged toward the nozzle mounting member by an elastic member interposed between the other end of the pin and the nozzle mounting member. °C
1. A support structure for a radial turbine nozzle, characterized in that the flange is attached to the nozzle attachment member.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP18214181U JPS5886405U (en) | 1981-12-09 | 1981-12-09 | Radial turbine nozzle support structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP18214181U JPS5886405U (en) | 1981-12-09 | 1981-12-09 | Radial turbine nozzle support structure |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5886405U true JPS5886405U (en) | 1983-06-11 |
Family
ID=29980243
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP18214181U Pending JPS5886405U (en) | 1981-12-09 | 1981-12-09 | Radial turbine nozzle support structure |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5886405U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2014037828A (en) * | 2012-08-14 | 2014-02-27 | General Electric Co <Ge> | Turbine aperture cap system |
-
1981
- 1981-12-09 JP JP18214181U patent/JPS5886405U/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2014037828A (en) * | 2012-08-14 | 2014-02-27 | General Electric Co <Ge> | Turbine aperture cap system |
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